Normal Shock Wave Turbulent Boundary Layer Interaction Control Using "Smart" Piezoelectric Flap Actuators
Proceedings, Aerospace aerodynamics research conference ; 2004 ; London
Aerospace aerodynamics research conference ; Paper 13-18
01.01.2004
Paper 13-18
Shelved in Conference Index.; Held on CD-ROM
Aufsatz (Konferenz)
Englisch
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Normal shock wave-turbulent boundary-layer interaction control using 'smart' piezoelectric actuators
Online Contents | 2005
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